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MITC finite elements for laminated composite plates
Author(s) -
Alfano G.,
Auricchio F.,
Rosati L.,
Sacco E.
Publication year - 2001
Publication title -
international journal for numerical methods in engineering
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 1.421
H-Index - 168
eISSN - 1097-0207
pISSN - 0029-5981
DOI - 10.1002/1097-0207(20010130)50:3<707::aid-nme55>3.0.co;2-1
Subject(s) - composite number , finite element method , structural engineering , boundary value problem , plane stress , stress (linguistics) , shear (geology) , extensional definition , transverse plane , mathematical analysis , geometry , mathematics , materials science , composite material , engineering , paleontology , linguistics , philosophy , biology , tectonics
Within the framework of the first‐order shear deformation theory, 4‐ and 9‐node elements for the analysis of laminated composite plates are derived from the MITC family developed by Bathe and coworkers. To this end the bases of the MITC formulation are illustrated and suitably extended to incorporate the laminate theory. The proposed elements are locking‐free, they do not have zero‐energy modes and provide accurate in‐plane deformations. Two consecutive regularizations of the extensional and flexural strain fields and the correction of the resulting out‐of‐plane stress profiles necessary to enforce exact fulfillment of the boundary conditions are shown to yield very satisfactory results in terms of transverse and normal stresses. The features of the proposed elements are assessed through several numerical examples, either for regular and highly distorted meshes. Comparisons with analytical solutions are also shown. Copyright © 2001 John Wiley & Sons, Ltd.